装甲的防护机理,需要结合装甲材料以及防护结构,进行综合考虑。 材料的选用以钛合金为例,在钛合金单独作为靶板时,其防护性能较弱。为提高靶板的抗弹性能,需要了解其失效特征与相应的损伤机理。常见的宏观损伤特征为冲塞、花瓣状变形、锥形断裂、背部崩落、背凸等。其中,锥形断裂表明靶板受到钝头弹体的冲击时,在局部拉应力的影响下,靶板表面上的初始缺陷逐步扩展为圆锥型裂纹,并在弹体向前动量的驱动下在材料中剪切分离出一个完整锥形体的宏观失效特征。与层裂的机理相似,这两者都是材料在强冲击载荷下的典型动态拉伸破坏模式。目前国内外关于层裂的相关研究很多,层裂现象的形成过程与微观机制也较为清晰。然而对于锥形断裂现象,针对其微观机制还需要国内外的进一步研究。 装甲防护的结构效应有多种,当前研究较多的结构效应有倾角效应、厚度效应、界面效应等。针对不同的弹体种类和装甲结构,装甲的结构效应对于抗弹性能的影响往往表现出不同的规律,对于特定的弹体及装甲结构其结构效应规律有待于进一步讨论。
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装甲防护机理
文献1(2017):Study on Protection Mechanism of 30CrMnMo-UHMWPE Composite Armor(30CrMnMo-UHMWPE复合装甲防护机理研究)

The node velocities and the element equivalent plastic strain in various parts(see Figure 6)are plotted to reveal the relationship between the velocity and the deformation in different parts of the projectile. These velocities at a typical time of 6 μs are plotted along a local coordinate, which describes the distance from the tail to the nose along the medial axis of the projectile. Owing to erosion during penetration, the length of the projectile is reduced to 35 mm. The plastic strain is zero for lengths of 0-22 mm, indicating that only elastic deformation occurs and, hence, the high initial values(-1798 m/s) of the node velocities are maintained. Owing to the elastic waves, however, the velocity fluctuates significantly near the nose. Furthermore, at projectile lengths of 22-35 mm, the equivalent plastic strain values of the projectile elements increase gradually from 0.006, and the speed of the corresponding nodes decreases significantly. The velocity of the nose decreases to a minimum of 784 m/s when the plastic strain reaches a maximum of 1.71. In stage I, the low-velocity regions correspond closely to the plastically deformed regions in the nose of the projectile.
Figure.6. Simulation results at 6 us.(a)Contours of equivalent plastic strain;and(b) node velocities d the corresponding element equivalent plastic strains.
The internal energy and mass loss of the steel and PE laminate are plotted for times ranging from 0 to 60μs, to determine the energy absorption of each layer during the projectile-target interactions. When the fragment penetrates the steel plate, the internal energy of the plate increases from zero reaching a maximum of 0.82 kJ at 13μs, decreases to 0.69 kJ at 18μs, and remains approximately constant thereafter. The subsequent constant mass loss shows that the plate stops the absorption of kinetic energy. Before the projectile reaches the PE laminate, the internal energy of the laminate increases continuously, reaching a maximum value (1.43 kJ) at 60μs. This value accounts for 68% of the total energy absorption of the target armor. Therefore, the PE laminate in the composite-structure armor plays an important role in the absorption of projectile kinetic energy during the penetration process.
Figure.9. Internal energy and mass loss of the steel and PE laminate for times ranging from 0 to 60μs.

Study on Protection Mechanism of 30CrMnMo-UHMWPE Composite Armor
Materials 2017 10(4):405-

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